Enhancement of cockpit external visibility

• US 8,952,831 B2
• Filed: 12/07/2012
• Issued: 02/10/2015
• Est. Priority Date: 12/07/2012
• Status: Expired due to Fees

• Current Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Original Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Inventors: Van Staagen, Michael G.
• Primary Examiner(s): BLOUNT, ERIC
• Application Number:
  US13/708,001
• Publication Number:
  US 20140159926A1
• Time in Patent Office: 795 Days
• Field of Search: 340/971, 340/945, 340/946, 701/3
• US Class Current: 340/971
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration

Abstract

A cockpit display system for a cockpit of an aircraft includes a primary flight display moveably located in the cockpit and viewable from a pilot position and/or a copilot position in the cockpit. The primary flight display is movable from a first position utilized for a first operating condition of the aircraft to a second position to increase external visibility during a second operating condition of the aircraft. A cockpit system includes a pilot operating position and a first flight display moveably located in the cockpit and viewable from the pilot operating position. The first flight display is movable from a first position utilized during a first operating condition of the aircraft to a second position to increase external visibility from the pilot operating position during a second operating condition of the aircraft.

Claims

1. A cockpit display system for a cockpit of an aircraft comprising:

a primary flight display disposed in the cockpit and viewable from a pilot position and/or a copilot position in the cockpit; and

a center console located between the pilot position and the copilot position, the primary flight display being movably connected to the center console;

wherein the primary flight display is movable from a first position utilized for a first operating condition of the aircraft to a second position to increase external visibility during a second operating condition of the aircraft.

2. The cockpit display system of claim 1, wherein the primary flight display is movable via a linkage assembly connected to the primary flight display.

3. The cockpit display system of claim 2, further comprising an actuator operably connected to the linkage assembly to drive movement of the primary flight display.

4. The cockpit display system of claim 1, wherein moving the primary flight display from the first position to the second position comprises moving the primary flight display closer to the center console.

5. The cockpit display system of claim 1, wherein a primary flight display located at the copilot position is viewable from the pilot position when in the first position, but is obstructed from viewing from the pilot position by the center console when the primary flight display is in the second position.

6. A cockpit system comprising:

a pilot operating position and a copilot operating position;

a center console located between the pilot operating position and the copilot operating position;

a first flight display moveably disposed in the cockpit and viewable from the pilot operating position;

a second flight display moveably disposed in the cockpit and viewable from the copilot operating position;

wherein the first flight display is movable from a first position utilized during a first operating condition of the aircraft to a second position to increase external visibility from the pilot operating position during a second operating condition of the aircraft; and

wherein the second flight display is movable from a first position utilized during the first operating condition of the aircraft to a second position to increase external visibility from the pilot operating position during a second operating condition of the aircraft.

7. The cockpit system of claim 6, wherein the first flight display is movable via a linkage assembly connected to the first flight display.

8. The cockpit system of claim 7, further comprising an actuator operably connected to the linkage assembly to drive movement of the first flight display.

9. The cockpit system of claim 6, further comprising a center console located between the pilot operating position and the copilot operating position.

10. The cockpit system of claim 6, wherein the first flight display and/or the second flight display is moveably connected to the center console.

11. The cockpit system of claim 6, wherein moving the first flight display from the first position to the second position comprises moving the first flight display closer to the center console.

12. The cockpit system of claim 6, wherein a second flight display located is viewable from the pilot operating position when in the first position, but is obstructed from viewing from the pilot operating position by the center console when the second flight display is in the second position.